Garmin G1000 Pilot’s Guide for Piper PA32 190-00692-00 Rev. B3-2ENGINE INDICATION SYSTEM3.1 EIS DISPLAYNOTE: The Fuel Quantity Indicator displays only to 50 gallons per side when full.The EIS Display shows all critical engine, fuel, and electrical indicators at the left of the MFD. In reversionarymode, the Engine Display is identical to the EIS Display normally shown on the MFD.1 Engine Manifold PressureGauge (MAN IN)Displays manifold pressure in inches of Mercury (in Hg) to indicate engine powerTurbocharged Aircraft – Maximum manifold pressure range displayed in red2 Tachometer (RPM) Displays propeller speed in revolutions per minute (rpm); the red rangeindicates propeller overspeed3 Fuel Quantity Indicator(FUEL QTY GAL)Displays the amount of fuel in gallons (gal) for each tank, labeled ‘L’ (left)and ‘R’ (right)4 Fuel Flow Indicator(FFLOW GPH)Displays fuel flow in gallons per hour (gph)5 Oil Temperature Indicator(OIL °F)Displays oil temperature in degrees Fahrenheit (°F)6 Oil Pressure Indicator(OIL PSI)Displays oil pressure in pounds per square inch (psi)7 Exhaust Gas TemperatureIndicator (EGT °F)Normally-aspirated AircraftDisplays exhaust gas temperature (EGT) of the hottest cylinder in °F8 Turbine Inlet TemperatureIndicator (TIT °F)Turbocharged AircraftDisplays the temperature at the turbine inlet in °F9 Cylinder Head TemperatureIndicator (CHT °F)Displays the temperature of the hottest cylinder in °F10 Emergency Battery Voltage(EMER BATT)Displays voltage for the emergency battery11 Essential Bus Voltage(ESS BUS)Displays voltage for the essential bus12 Main Alternator Current(MAIN ALT)Displays main alternator current in amperes (A)If the main alternator fails, changes to display standby alternator current
